20020822021999A

Accident · Substantial damage

FAA accident report · Airtrc AT-301 · Dospalos, CA · August 22, 2002

Date
August 22, 2002 · 07:15 local
Place
Dospalos, CA
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N8793S
NTSB investigation
NTSBLAX02LA257
Reported as
Airtrc AT301

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) One propeller blade failed/loss of a portion of the blade. Engine vibration caused failure of the engine mount. The p&w R1340 engine separated from the airframe at touch down in an open field. (.19) on August 22, 2002, at 0700 pacific daylight time, an air tractor AT-301, N8793S, made a forced landing in a newly disked field after losing a portion of a propeller blade, and came to rest inverted. The airplane, operated by spain air under the provisions of 14 CFR part 137 as a crop dusting operation, sustained substantial damage. The commercial pilot, the sole occupant, was not injured. Visual metrological conditions prevailed for the local area flight and no flight plan had been filed. The flight departed a private airstrip about 0650. According to the pilot, he had been crop dusting since midnight. There were no mechanical anomalies noted during that time. On the accident flight part of the propeller blade came off. The pilot stated that the engine started to vibrate and he made an emergency landing in a cotton field. On the landing rollout the landing gear caught on the soft dirt and the airplane nosed over inverted.

As the FAA filed it

(-23) ONE PROPELLER BLADE FAILED/LOSS OF A PORTION OF THE BLADE. ENGINE VIBRATION CAUSED FAILURE OF THE ENGINE MOUNT. THE P&W R1340 ENGINE SEPARATED FROM THE AIRFRAME AT TOUCH DOWN IN AN OPEN FIELD. (.19) ON AUGUST 22, 2002, AT 0700 PACIFIC DAYLIGHT TIME, AN AIR TRACTOR AT-301, N8793S, MADE A FORCED LANDING IN A NEWLY DISKED FIELD AFTER LOSING A PORTION OF A PROPELLER BLADE, AND CAME TO REST INVERTED. THE AIRPLANE, OPERATED BY SPAIN AIR UNDER THE PROVISIONS OF 14 CFR PART 137 AS A CROP DUSTING OPERATION, SUSTAINED SUBSTANTIAL DAMAGE. THE COMMERCIAL PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. VISUAL METROLOGICAL CONDITIONS PREVAILED FOR THE LOCAL AREA FLIGHT AND NO FLIGHT PLAN HAD BEEN FILED. THE FLIGHT DEPARTED A PRIVATE AIRSTRIP ABOUT 0650. ACCORDING TO THE PILOT, HE HAD BEEN CROP DUSTING SINCE MIDNIGHT. THERE WERE NO MECHANICAL ANOMALIES NOTED DURING THAT TIME. ON THE ACCIDENT FLIGHT PART OF THE PROPELLER BLADE CAME OFF. THE PILOT STATED THAT THE ENGINE STARTED TO VIBRATE AND HE MADE AN EMERGENCY LANDING IN A COTTON FIELD. ON THE LANDING ROLLOUT THE LANDING GEAR CAUGHT ON THE SOFT DIRT AND THE AIRPLANE NOSED OVER INVERTED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.